R.530
From Wikipedia, the free encyclopedia
Matra R.530 | |
---|---|
An R530 exhibited at the South African Air Force Museum, Swartkop | |
Type | short-range air-to-air missile |
Service history | |
In service | 1962 [1] |
Production history | |
Manufacturer | Matra |
Specifications | |
Weight | 192 kg [1] |
Length | 3.28 m [1] |
Diameter | 263 mm [1] |
| |
Engine |
two stage solid rocket,[1] Hotchkiss-Brandt/SNPE Antoinette rocket [2] 83.3 kN for 2.7 s + 6.5 s cruise[2] |
Wingspan | 1.1 m[2] |
Operational range | 1.5 to 20 km [1] |
Speed | Mach 2.7 [1] |
Guidance system | Radar and IR [3] |
Launch platform |
Dassault Mirage F1 Dassault Mirage III [1] F-8 Crusader |
The Matra R.530 is a French medium to short range air-to-air missile. It was available in IR (passive infrared) and SARH as the main armament of the Mirage III which was able to carry a single missile in the centerline, the Mirage F1, which carried 2 (1 of each type) under the wings, and the F-8 Crusader in the French Navy service.
Operators
- Argentina
- Australia
- Brazil
- Cameroon
- Colombia
- France
- Egypt
- Iraq
- Israel
- Jordan
- Lebanon
- Morocco
- Pakistan
- South Africa
- Spain
- Venezuela
See also
References
External links
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.